Flows past airfoils for the low-Reynolds number conditions of flying in Martian atmosphere-Reference-Cited by-同舟云学术

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Flows past airfoils for the low-Reynolds number conditions of flying in Martian atmosphere

Published:2024-08 Issue: Volume:221 Page:94-107
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Aprovitola Andrea,Iuspa Luigi^ORCID,Pezzella Giuseppe^ORCID,Viviani Antonio^ORCID

Publisher

Elsevier BV

Reference45 articles.

1. A system engineering approach to the conceptual design of a martian uav;D’Urso,2016

2. Design of the ARES Mars airplane and mission architecture;Braun;J. Spacecr. Rockets,2006

3. Mars helicopter technology demonstrator;Balaram,2018

4. Mars: An Introduction to Its Interior, Surface and Atmosphere;Barlow,2014

5. Vision and Voyages for Planetary Science in the Decade 2013–2022;National Research Council,2021

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic performance optimization of a UAV's airfoil at low-Reynolds number and transonic flow under the Martian carbon dioxide atmosphere;Acta Astronautica;2024-10

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